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Passed
gpkit.tests.from_paths.TestFiles.test_SPaircraft_py_mosek_cli (from gpkit.tests.from_paths.TestFiles-20200715061911)
Standard Output
Starting a sequence of GP solves for 317 free variables in 136 locally-GP constraints and for 1198 free variables in 4705 posynomial inequalities. GP Solve 1 Using solver 'mosek_cli' for 1198 free variables in 4705 posynomial inequalities. Solving took 0.306 seconds. Solved cost was 3.965e+40. GP Solve 2 Using solver 'mosek_cli' for 1198 free variables in 4705 posynomial inequalities. Solving took 0.26 seconds. Solved cost was 4.009e+10. GP Solve 3 Using solver 'mosek_cli' ...[truncated 8466 chars]... 9585682962033] dimensionless Fuselage Cd Percent Diff: [108.78752887] VT Cd Percent Diff: [-35.47524300932485] dimensionless Wing Cd percent Diff: [-29.70499848] Induced Drag Cd Percent Diff: [-33.71254764] CRUISE SEGMENT 1 TSFC DIFFERENCES Initial Cruise TSFC Percent Diff: [-5.63063796] FUSELAGE DIFFERENCES Weight of HB material: -48.57964106717352 Weight of VB material: 117.19786145169972 Fan Propulsive Efficiency in Cruise Segment 1 --------------------- [0.80257716]
Standard Error
/Users/jenkins/workspace/CE_gplibrary_Push_research_models/mosek/gpkit/gpkit/constraints/gp.py:407: RuntimeWarning: divide by zero encountered in log for i, mi in enumerate(self.m_idxs) if la[i])